{"created":"2023-06-20T15:08:26.116009+00:00","id":37884,"links":{},"metadata":{"_buckets":{"deposit":"6b342c1d-68e2-44c9-829c-372082a44370"},"_deposit":{"created_by":1,"id":"37884","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"37884"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00037884","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["430758","430759"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Dependency of a boundary layer flow on computational grids"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1994-12","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"320","bibliographicPageStart":"315","bibliographicVolumeNumber":"27","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所特別資料"},{"bibliographic_title":"Special Publication of National Aerospace Laboratory","bibliographic_titleLang":"en"}]}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"層流から乱流への遷移を数値的に予測する第一歩として層流境界層に関し線形安定解析を行った。計算機と高精度計算スキームの発達によって境界層を計算するのに境界層方程式でなくナビエ･ストークス方程式に基くコードを用いることができる。したがって、ナビエ･ストークスコードによって計算された境界層の精度を検証することは意義がある。無限後退円柱のまわりの超音速流れを密度の異なる3種の格子により計算し、格子密度に依存しない正確な速度や温度のプロファイルを得るのにどの程度の格子数が必要かを調べた。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The first step to numerically predict laminar-turbulent transition is taken by the linear stability analysis on a laminar boundary layer. Presently the improvements of high-accuracy schemes as well as computers have enabled Navier-Stokes code to calculate the boundary layer instead of a boundary layer code. It is therefore significant to verify the accuracy of the boundary layer calculated by Navier-Stokes code. By simulating a supersonic flow around an infinite swept cylinder with three kinds of grids which differ in density, it is investigated how many cells are needed in the boundary layer to obtain the accurate velocity and temperature profiles independent of grid density.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0004174047","subitem_description_type":"Other"}]},"item_5_description_33":{"attribute_name":"レポート番号","attribute_value_mlt":[{"subitem_description":"レポート番号: NAL SP-27","subitem_description_type":"Other"}]},"item_5_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"航空宇宙技術研究所"}]},"item_5_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"National Aerospace Laboratory (NAL)"}]},"item_5_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0289-260X","subitem_source_identifier_type":"ISSN"}]},"item_5_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AN10097345","subitem_source_identifier_type":"NCID"}]},"item_5_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"航空宇宙技術研究所"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"野村, 聡幸"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nomura, Toshiyuki","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_files":{"attribute_name":"ファイル情報","attribute_type":"file","attribute_value_mlt":[{"accessrole":"open_date","date":[{"dateType":"Available","dateValue":"2020-01-24"}],"displaytype":"detail","filename":"nalsp0027047.pdf","filesize":[{"value":"328.7 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0027047.pdf","url":"https://jaxa.repo.nii.ac.jp/record/37884/files/nalsp0027047.pdf"},"version_id":"4c030755-35b4-4e5c-b389-0350a24f88a8"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"超音速流れ","subitem_subject_scheme":"Other"},{"subitem_subject":"乱流遷移","subitem_subject_scheme":"Other"},{"subitem_subject":"境界層流れ","subitem_subject_scheme":"Other"},{"subitem_subject":"円柱","subitem_subject_scheme":"Other"},{"subitem_subject":"安定解析","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD検証","subitem_subject_scheme":"Other"},{"subitem_subject":"格子密度","subitem_subject_scheme":"Other"},{"subitem_subject":"超音速境界層","subitem_subject_scheme":"Other"},{"subitem_subject":"速度分布","subitem_subject_scheme":"Other"},{"subitem_subject":"温度分布","subitem_subject_scheme":"Other"},{"subitem_subject":"ナビエ･ストークスコード","subitem_subject_scheme":"Other"},{"subitem_subject":"数値シミュレーション","subitem_subject_scheme":"Other"},{"subitem_subject":"計算格子","subitem_subject_scheme":"Other"},{"subitem_subject":"supersonic flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"transition to turbulence","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"boundary layer flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"cylinder","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"stability analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD validation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"grid density","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"supersonic boundary layer","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"velocity distribution","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"temperature distribution","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Navier Stokes code","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"numerical simulation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"computational grid","subitem_subject_language":"en","subitem_subject_scheme":"Other"}]},"item_language":{"attribute_name":"言語","attribute_value_mlt":[{"subitem_language":"jpn"}]},"item_resource_type":{"attribute_name":"資源タイプ","attribute_value_mlt":[{"resourcetype":"conference paper","resourceuri":"http://purl.org/coar/resource_type/c_5794"}]},"item_title":"境界層流れの計算格子に対する依存性","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"境界層流れの計算格子に対する依存性"}]},"item_type_id":"5","owner":"1","path":["1891","1915"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"37884","relation_version_is_last":true,"title":["境界層流れの計算格子に対する依存性"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T22:47:05.967473+00:00"}